曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
the data for format and acceptability.
If data is not accepted, a specific message appears
in white on the scratchpad:FORMAT ERROR or NOT IN DATA
BASE or NOT ALLOWED or ENTRY OUT OF RANGE.
NOTES: - Data entry in amber boxes is mandatory and
white dashed lines indicate that data will be
calculated and displayed by the FMGC when it
has enough information to do so.
- The scratchpad is limited to a maximum of 22
characters.
TMUFM2403-T04 LEVEL 3
EFFECTIVITY 22-82-00 Page 8
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 166
ALL
MCDU DESCRIPTION - DISPLAY LAYOUT / DATA ENTRY
TMUFM2403-P04 LEVEL 3
EFFECTIVITY 22-82-00 Page 9
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 167
ALL
MCDU DESCRIPTION
COLOR MODE
- Titles, comments, dashes, symbols and minor messages
are displayed in white.
- Non modifiable data or active data are displayed in
green.
However, in temporary flight plan, the same data are
shown in yellow until they are validated by an
insertion.
- The modifiable data and selectable data are displayed
in cyan.
- Mandatory data, boxes, required pilot actions and
important messages are displayed in amber.
- The maximum recommended Flight Level is indicated
in magenta.
- Data associated to the flight plan constraints are
also indicated in magenta.
An asterix (*) displayed adjacent to the corresponding
altitude or airspeed restriction is amber to indicate
"missed" or magenta to indicate "made".
TMUFM2403-T05 LEVEL 3
EFFECTIVITY 22-82-00 Page 10
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 168
ALL
MCDU DESCRIPTION - COLOR MODE
TMUFM2403-P05 LEVEL 3
EFFECTIVITY 22-82-00 Page 11
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 169
ALL
SELF EXAMINATION
The Multipurpose Control and Display Unit (MCDU) is:
A - the pilot interface with the Flight
Management function of the FMGC.
B - the aircraft interface between the
Flight Management and Flight Guidance
functions of the FMGC.
C - an independent means of controlling the
aircraft in manual flight.
What is the purpose of the white MCDU MENU
annunciator light?
A - It alerts the crew that the MCDU has
failed.
B - A system, linked to the MCDU, requests
the display.
C - It alerts the crew that the MCDU MENU
page is not available.
What is the correct statement?
A - Line Select Keys may be used to transfer
data onto the scratchpad.
B - Modifiable data must first be entered
onto the scratchpad before being
transferred, by using the appropriate
Line Select Key.
C - Line Select Keys may be used to delete
data from the adjacent data field,
without using the CLR key.
TMUFM2403 LEVEL 3
EFFECTIVITY 22-82-00 Page 12
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 170
ALL
22 - AUTO FLIGHT SYSTEM
22-75-00 EFIS DISPLAY
CONTENTS:
Flight Management (FM) Display on PFD
Flight Management (FM) Display on ND
Data Base Display P/Bs
Flight Management (FM) Source Switching
MCDU Failure
Self Examination
TMUFM0504 LEVEL 3
EFFECTIVITY 22-75-00 Page 1
Jul 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 171
ALL
EFIS DISPLAY
FLIGHT MANAGEMENT (FM) DISPLAY ON PFD
The Primary Flight Display (PFD), as main guidance
instrument, displays the data computed, or inserted
on the Multipurpose Control and Display Unit (MCDU).
This data can be the target speed and the altitude
constraint in managed guidance modes, V1 and V2,
Decision Height (DH) or Minimum Decision Altitude (MDA)
in approach.
At the top of the PFD, the Flight Mode Annunciator
(FMA) provides the pilot with the DH or the MDA.
The speed scale displays the Flight Management data
such as the target speed and V1.
The altitude scale displays the altitude constraint
from the Flight Management (FM) part and the linear
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
ATA 22 AUTO FLIGHT SYSTEM(34)
